EP2936656B1 - Rotor assembly having a functional carrier - Google Patents
Rotor assembly having a functional carrier Download PDFInfo
- Publication number
- EP2936656B1 EP2936656B1 EP13810933.5A EP13810933A EP2936656B1 EP 2936656 B1 EP2936656 B1 EP 2936656B1 EP 13810933 A EP13810933 A EP 13810933A EP 2936656 B1 EP2936656 B1 EP 2936656B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- rotor
- section
- winding
- web
- support element
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000004804 winding Methods 0.000 claims description 29
- 238000009413 insulation Methods 0.000 claims description 9
- 230000005520 electrodynamics Effects 0.000 claims description 4
- 239000000463 material Substances 0.000 claims description 4
- 238000003475 lamination Methods 0.000 claims 6
- 239000002184 metal Substances 0.000 description 10
- 229910052751 metal Inorganic materials 0.000 description 10
- 238000000034 method Methods 0.000 description 3
- 239000004033 plastic Substances 0.000 description 3
- 229920003023 plastic Polymers 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229920000965 Duroplast Polymers 0.000 description 1
- 239000004638 Duroplast Substances 0.000 description 1
- 238000005538 encapsulation Methods 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
- 238000005491 wire drawing Methods 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K3/00—Details of windings
- H02K3/46—Fastening of windings on the stator or rotor structure
- H02K3/50—Fastening of winding heads, equalising connectors, or connections thereto
- H02K3/51—Fastening of winding heads, equalising connectors, or connections thereto applicable to rotors only
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K3/00—Details of windings
- H02K3/32—Windings characterised by the shape, form or construction of the insulation
- H02K3/34—Windings characterised by the shape, form or construction of the insulation between conductors or between conductor and core, e.g. slot insulation
- H02K3/345—Windings characterised by the shape, form or construction of the insulation between conductors or between conductor and core, e.g. slot insulation between conductor and core, e.g. slot insulation
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K3/00—Details of windings
- H02K3/32—Windings characterised by the shape, form or construction of the insulation
- H02K3/38—Windings characterised by the shape, form or construction of the insulation around winding heads, equalising connectors, or connections thereto
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K3/00—Details of windings
- H02K3/46—Fastening of windings on the stator or rotor structure
- H02K3/52—Fastening salient pole windings or connections thereto
- H02K3/527—Fastening salient pole windings or connections thereto applicable to rotors only
Definitions
- a disadvantage of these rotors according to the prior art is that there is no sufficient protection against the relatively high wire tension, which is necessary when winding the rotor coils, and acts on the winding posts. This wire pull may cause deformation or even breakage of the winding supports at the ends of the rotor core.
- the end plate member may be positioned at the first rotor end.
- a further Endblechelement may be positioned at the second end of the rotor.
- the Endblechelement can be connected by a frictional connection, form-fitting or material connection with the rotor package.
- the support member includes a first portion and a second portion, wherein the first portion extends substantially in a first plane and the second portion substantially in a further plane perpendicular to the extending first plane and in the direction of a rotor end.
- the support element may be configured in the form of a curved contour, wherein in each case a free end of the support element extends in the direction of a rotor end. Due to this particular embodiment of the support element, a stress concentration in the interface between the first and second sections can be effectively avoided.
- the Endblechelement may be formed of a higher-strength material.
- Fig. 1 and 2 show a rotor 1 for an electrodynamic machine, in particular for an electric motor.
- the rotor 1 consists essentially of a rotor core 10, a bar insulation (not shown) and an end plate element 40.
- the rotor core 10 is composed of a plurality of individual sheet metal rings 20, which are fixedly connected to each other, whereby the rotor 1 and the rotor core 10 is given a substantially cylindrical shape. Furthermore, the rotor core 10 has an outer surface 12, an inner surface 14 and a first rotor end 16 and a second rotor end 18.
- the individual sheet metal rings 20 have a star-shaped shape with twenty-four evenly distributed web elements 22, which extend radially outwards from a central passage opening 24 of the rotor core 10.
- the individual web elements 22 When the individual sheet metal rings 20 are connected to the rotor core, the individual web elements 22 together form twenty-four continuous webs 30 which extend along the outer surface 12 of the rotor core 10 over its entire length of the rotor core 10 (cf. Fig. 2 ). The webs 30 form the rotor poles.
- the rotor core 10 is in the form of a cylinder with the central passage opening 24.
- the passage opening 24 serves to receive a drive shaft 32, which passes on the speed generated by the electric motor or the torque generated for use.
- the bar insulation (not shown) is in the form of a cylindrical tube having a first end, a second end, an inner surface, and an outer surface.
- the web insulation On the outer surface, the web insulation has twenty-four uniformly distributed winding support elements, which extend radially outward.
- the winding support elements enclose the webs 30 of the rotor core 10 and have an elongate base body with a carrier plate.
- Each coil support member is wound with a wire (not shown) (e.g., copper wire) into a rotor coil.
- the wire not shown, is wound several times around the elongated base body and below the support plate of the winding support element.
- the Endblechelement 40 substantially corresponds to the shape of a sheet-metal ring 20 in the form of a twenty-four-pointed star.
- the Endblechelement 40 in turn contains twenty-four uniformly distributed individual support elements 50, which extend radially outwards.
- the support elements 50 in turn consist of a first portion 60 and a second portion 70.
- the first portion 60 extends radially outward.
- the second section 70 extends at a right angle to the first section 60, pointing in the direction of the rotor end 16.
- the Endblechelement 40 is partially an integral part of the (not shown) web insulation. As in Fig. 1 the Endblechelement 40 is positioned in the direction A or in the direction B to the first rotor end 16 and to the second rotor end 18, so that each end plate member 40 abut the respective rotor ends 16, 18 area.
- the first section 60 of each of the twenty-four support elements 50 is attached to the end face of a corresponding web 30.
- the second section 70 of the twenty-four support elements 50 extends in the direction of the first rotor end 16 or correspondingly in the direction of the second rotor end 18.
- each of the twenty-four coil support members (not shown) of the bridge insulation each surrounds one of the ridges 30 of the rotor pack 10.
- one coil winding wire (not shown) is wound.
- the first section 60 of the twenty-four support elements 50 of the Endblechelements 40 is thus located between the end face of the webs 30 of the rotor core 10 and the winding support elements of the web insulation.
- the first portion 60 of the support elements 50 supports the webs 30 against the axially acting forces, which are generated by the wire of the winding.
- the second portion 70 of the support members 50 is integrated into the front end (ie, which is in the direction of the first rotor end 16 and in the direction of the second rotor end 18) of the support plate of the winding support elements, thereby the ends of this support plate against the radially acting forces of To support wire pull of the winding.
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Insulation, Fastening Of Motor, Generator Windings (AREA)
- Windings For Motors And Generators (AREA)
Description
Die Erfindung betrifft einen Rotor für eine elektrodynamische Maschine, insbesondere einen Elektromotor. Der Rotor enthält ein Rotorpaket mit einem ersten Rotorende und einem zweiten Rotorende sowie einer Vielzahl miteinander verbundener Blechringe. Jeder Blechring enthält wenigstens ein Stegelement. Die einzelnen Stegelemente formen in Reihe zueinander positioniert einen Steg. Des Weiteren enthält der Rotor eine Stegisolation mit zumindest einem Wickelstützelement zur Aufnahme einer Rotorspule.The invention relates to a rotor for an electrodynamic machine, in particular an electric motor. The rotor includes a rotor core having a first rotor end and a second rotor end and a plurality of interconnected metal rings. Each sheet metal ring contains at least one web element. The individual web elements form a web positioned in series with each other. Furthermore, the rotor includes a web insulation with at least one winding support element for receiving a rotor coil.
Üblicherweise besteht ein Rotor bzw. Läufer, Anker, Induktor oder Polrad für einen Elektromotor unter anderem aus einem Rotorpaket. Das Rotorpaket wird hierzu aus einzelnen Blechringen gebildet. Dazu verfügt das Rotorpaket über eine Anzahl an Rotorpolen bzw. Stege, welche sich radial in das Innere des Rotorpakets erstrecken. Zwischen den einzelnen Rotorpolen befinden sich dabei Zwischenräume in Form von Polnuten.Usually there is a rotor or rotor, armature, inductor or rotor for an electric motor, inter alia, from a rotor package. The rotor core is formed from individual sheet metal rings. For this purpose, the rotor package has a number of rotor poles or webs, which extend radially into the interior of the rotor package. Between the rotor poles there are gaps in the form of Polnuten.
Gewöhnlich wird die Innenfläche des Rotorpakets, die Rotorpole sowie die Polnuten mit einem Kunststoff umspritzt bzw. ummantelt. Alternativ können die Polnuten auch mit Papier isoliert werden. Bei dem Kunststoff kann es sich beispielsweise um Polymere, wie z.B. Duroplast oder Thermoplast, handeln. Die Kunststoff-Umspritzung formt dabei jeweils um die einzelnen Rotorpole die eigentlichen Wickelstützen, welche zur Aufnahme der Rotorspulen dienen.Usually, the inner surface of the rotor package, the rotor poles and the Polnuten is encapsulated with a plastic or coated. Alternatively, the Polnuten can also be isolated with paper. The plastic may be, for example, polymers, e.g. Duroplast or thermoplastic, act. The plastic encapsulation forms each of the individual rotor poles the actual winding posts, which serve to accommodate the rotor coils.
Ein Nachteil an diesen Rotoren gemäss dem Stand der Technik besteht darin, dass kein ausreichender Schutz gegen den relativ hohen Drahtzug vorgesehen ist, welcher beim Wickeln der Rotorspulen notwendig ist, und auf die Wickelstützen wirkt. Durch diesen Drahtzug kann es zu einer Verformung oder sogar zu einem Abbrechen der Wickelstützen an den Enden des Rotorpakets kommen.A disadvantage of these rotors according to the prior art is that there is no sufficient protection against the relatively high wire tension, which is necessary when winding the rotor coils, and acts on the winding posts. This wire pull may cause deformation or even breakage of the winding supports at the ends of the rotor core.
Das Dokument
Eine Aufgabe der vorliegenden Erfindung besteht darin, die vorstehend genannten Probleme zu lösen und damit einen Rotor bereitzustellen, welcher auf einfache Art und Weise sowie kostengünstig den Anforderungen des Wickelprozesses, insbesondere den Anforderungen des hohen Drahtzugs, genügt.An object of the present invention is to solve the above-mentioned problems and thus to provide a rotor which satisfies the requirements of the winding process, in particular the requirements of the high wire tension, in a simple manner and cost-effectively.
Die Aufgabe wird erfindungsgemäss durch einen Rotor für eine elektrodynamische Maschine, insbesondere einen Elektromotor. Der Rotor enthält ein Rotorpaket mit einem ersten Rotorende und einem zweiten Rotorende sowie einer Vielzahl miteinander verbundener Blechringe. Jeder Blechring enthält wenigstens ein Stegelement. Die einzelnen Stegelemente formen in Reihe zueinander positioniert einen Steg. Des Weiteren enthält der Rotor eine Stegisolation mit zumindest einem Wickelstützelement zur Aufnahme einer Rotorspule.The object is achieved by a rotor for an electrodynamic machine, in particular an electric motor. The rotor includes a rotor core having a first rotor end and a second rotor end and a plurality of interconnected metal rings. Each sheet metal ring contains at least one web element. The individual web elements form a web positioned in series with each other. Furthermore, the rotor includes a web insulation with at least one winding support element for receiving a rotor coil.
Erfindungsgemäss ist mindestens ein Endblechelement mit wenigstens einem Abstützelement vorgesehen, wobei das Endblechelement wenigstens teilweise in dem Wickelstützelement angeordnet ist. Durch das zusätzlich vorhandene Endblechelement verfügen die Wickelstützelement an deren Enden über ausreichende Widerstandskraft gegen die relativ hohen Kräfte des Wickelprozesses, insbesondere des Drahtzuges.According to the invention, at least one end plate element is provided with at least one support element, wherein the end plate element is arranged at least partially in the winding support element. Due to the additionally present Endblechelement have the winding support member at the ends of sufficient resistance to the relatively high forces of the winding process, in particular the wire drawing.
Entsprechend einer alternativen Ausgestaltungsform der vorliegenden Erfindung kann das Endblechelement an dem ersten Rotorende positioniert sein. Darüber hinaus ist es jedoch auch möglich, dass ein weiteres Endblechelement an dem zweiten Rotorende positioniert sein kann. Das Endblechelement kann dabei durch eine Kraftschluss-, Formschluss- oder Stoffschlussverbindung mit dem Rotorpaket verbunden werden.According to an alternative embodiment of the present invention, the end plate member may be positioned at the first rotor end. In addition, however, it is also possible that a further Endblechelement may be positioned at the second end of the rotor. The Endblechelement can be connected by a frictional connection, form-fitting or material connection with the rotor package.
Gemäss einer weiteren vorteilhaften Ausgestaltung der vorliegenden Erfindung kann vorgesehen sein, dass das Abstützelement einen ersten Abschnitt sowie einen zweiten Abschnitt enthält, wobei sich der erste Abschnitt im Wesentlichen in einer ersten Ebene erstreckt und sich der zweite Abschnitt im Wesentlichen in einer weiteren Ebene rechtwinkelig zu der ersten Ebene sowie in Richtung eines Rotorendes erstreckt.According to a further advantageous embodiment of the present invention can be provided that the support member includes a first portion and a second portion, wherein the first portion extends substantially in a first plane and the second portion substantially in a further plane perpendicular to the extending first plane and in the direction of a rotor end.
Durch die rechtwinklig zueinander stehenden Abschnitte des Abstützelements ist eine Abstützung der Wickelstützelemente sowohl in radialer als auch in axialer Ausrichtung gegen die auftretenden Kräfte des Drahtzugs der Wickelung gewährleistet.Due to the mutually perpendicular sections of the support element, a support of the winding support elements is ensured both in the radial and in axial alignment against the forces of the Drahtzugs the winding.
Der erste Abschnitt des Abstützelements kann an einer Stirnseite des Stegs positioniert sein. Hierdurch ist sichergestellt, dass der erste Abschnitt des Abstützelements nicht zwischen den einzelnen Stegen herausragt und dadurch der Rotorwicklung im Wege ist.The first portion of the support element may be positioned on an end face of the web. This ensures that the first portion of the support element does not protrude between the individual webs and thereby the rotor winding is in the way.
Des Weiteren kann ein Versteifungselement zwischen dem ersten Abschnitt und dem zweiten Abschnitt vorgesehen sein, wodurch ein Verformen des ersten und zweiten Abschnitts zueinander verhindert und zusätzliche Stabilität erzeugt werden kann. Das Versteifungselement kann dabei in Form von zusätzlich aufgebrachtem Material zwischen dem ersten und zweiten Abschnitt ausgestaltet sein. Darüber hinaus kann das Versteifungselement auch als entsprechende Versteifungsrippe oder-vertiefung ausgestaltet sein.Further, a stiffening member may be provided between the first portion and the second portion, thereby preventing deformation of the first and second portions from each other and additional stability may be generated. The stiffening element may be in the form of additionally applied material between the first and second Be designed section. In addition, the stiffening element can also be designed as a corresponding stiffening rib or recess.
Gemäss einer weiteren Ausgestaltungsform der vorliegenden Erfindung kann das Abstützelement in Form einer gebogenen Kontur ausgestaltet sein, wobei sich jeweils ein freies Ende des Abstützelementes in Richtung eines Rotorendes erstreckt. Durch diese besondere Ausgestaltungsform des Abstützelements kann eine Stresskonzentration in der Schnittstelle zwischen dem ersten und zweiten Abschnitt effektiv vermieden werden.According to a further embodiment of the present invention, the support element may be configured in the form of a curved contour, wherein in each case a free end of the support element extends in the direction of a rotor end. Due to this particular embodiment of the support element, a stress concentration in the interface between the first and second sections can be effectively avoided.
Um dem Endblechelement eine besonders hohe Widerstandskraft und eine höhere Festigkeit gegen die relativ hohen Kräfte des Wickelprozesses, insbesondere des Drahtzuges, zu geben, kann das Endblechelement aus einem höherfesten Werkstoff gebildet sein.In order to give the Endblechelement a particularly high resistance and a higher strength against the relatively high forces of the winding process, in particular the wire, the Endblechelement may be formed of a higher-strength material.
Weitere Vorteile ergeben sich aus der folgenden Zeichnungsbeschreibung. In der Zeichnung ist ein Ausführungsbeispiel der vorliegenden Erfindung dargestellt. Die Zeichnung, die Beschreibung und die Ansprüche enthalten zahlreiche Merkmale in Kombination. Der Fachmann wird die Merkmale zweckmässigerweise auch einzeln betrachten und zu sinnvollen weiteren Kombinationen zusammenfassen.Further advantages emerge from the following description of the drawing. In the drawing, an embodiment of the present invention is shown. The drawing, the description and the claims contain numerous features in combination. The skilled person will conveniently consider the features individually and summarize meaningful further combinations.
Es zeigen:
- Fig. 1
- eine perspektivische Ansicht eines erfindungsgemässen Rotors mit einem Rotorpaket sowie einem Endblechelement auf einer Antriebswelle;
- Fig. 2
- eine Seitenansicht des erfindungsgemässen Rotors mit einem Rotorpaket sowie einem Endblechelement auf einer Antriebswelle;
- Fig. 3
- eine perspektivische Ansicht des Endblechelements auf einer Antriebswelle; und
- Fig. 4
- eine Frontansicht des Endblechelements.
- Fig. 1
- a perspective view of a rotor according to the invention with a rotor core and a Endblechelement on a drive shaft;
- Fig. 2
- a side view of the inventive rotor with a rotor core and a Endblechelement on a drive shaft;
- Fig. 3
- a perspective view of the Endblechelements on a drive shaft; and
- Fig. 4
- a front view of the Endblechelements.
Der Rotor 1 besteht im Wesentlichen aus einem Rotorpaket 10, einer (nicht gezeigten) Stegisolation und einem Endblechelement 40.The
Das Rotorpaket 10 setzt sich aus mehreren einzelnen Blechringen 20 zusammen, welche miteinander fest verbunden sind, wodurch dem Rotor 1 sowie dem Rotorpaket 10 eine im Wesentlichen zylindrische Form gegeben wird. Des Weiteren weist das Rotorpaket 10 eine Aussenfläche 12, eine Innenfläche 14 sowie ein erstes Rotorende 16 und ein zweites Rotorende 18 auf.The
Die einzelnen Blechringe 20 weisen eine sternförmige Form mit vierundzwanzig gleichmässig verteilten Stegelementen 22 auf, die sich von einer zentralen Durchgangsöffnung 24 des Rotorpakets 10 radial nach aussen erstrecken.The individual
Wenn die einzelnen Blechringe 20 zu dem Rotorpaket verbunden sind, bilden die einzelnen Stegelemente 22 zusammen vierundzwanzig durchgehende Stege 30, welche sich entlang der Aussenfläche 12 des Rotorpakets 10 über dessen gesamte Länge des Rotorpakets 10 erstrecken (vgl.
Durch die sternförmige Form der Blechringe 20 erhält das Rotorpaket 10 die Form eines Zylinders mit der zentralen Durchgangsöffnung 24. Die Durchgangsöffnung 24 dient zur Aufnahmen einer Antriebswelle 32, welche die durch den Elektromotor erzeugte Drehzahl bzw. das erzeugte Drehmoment zur Nutzung weitergibt.Due to the star-shaped shape of the sheet metal rings 20, the
Die (nicht gezeigte) Stegisolation ist in Form eines zylindrischen Rohrs mit einem ersten Ende, einem zweiten Ende, einer Innenfläche und einer Aussenfläche. An der Aussenfläche weist die Stegisolation vierundzwanzig gleichmässig verteilte Wickelstützelemente auf, welche sich radial nach Aussen erstrecken. Die Wickelstützelemente umschliessen die Stege 30 des Rotorpakets 10 und weisen einen länglichen Grundkörper mit einer Trägerplatte auf. Jedes Wickelstützelement wird jeweils mit einem nicht gezeigten Draht (z.B. Kupferdraht) zu einer Rotorspule umwickelt. Der nicht gezeigte Draht wird dabei mehrmals um den länglichen Grundkörper und unterhalb der Trägerplatte des Wickelstützelementes gewickelt.The bar insulation (not shown) is in the form of a cylindrical tube having a first end, a second end, an inner surface, and an outer surface. On the outer surface, the web insulation has twenty-four uniformly distributed winding support elements, which extend radially outward. The winding support elements enclose the
Wie in
Das Endblechelement 40 ist teilweise integraler Bestandteil der (nicht gezeigten) Stegisolation. Wie in
Wie bereits vorstehend beschrieben umschliesst jede der vierundzwanzig (nicht gezeigten) Wickelstützelemente der (ebenfalls nicht gezeigten) Stegisolation jeweils einen der Stege 30 des Rotorpakets 10. Um jede der vierundzwanzig Wickelstützelemente wird jeweils ein (nicht gezeigter) Draht für eine Spulenwicklung gewickelt. Der erste Abschnitt 60 der vierundzwanzig Abstützelemente 50 des Endblechelements 40 befindet sich damit zwischen der Stirnseite der Stege 30 des Rotorpakets 10 und den Wickelstützelementen der Stegisolation. Hierdurch stützt der erste Abschnitt 60 der Abstützelemente 50 die Stege 30 gegen die axial wirkenden Kräfte, welche durch den Drahtzug der Wicklung erzeugt werden.As already described above, each of the twenty-four coil support members (not shown) of the bridge insulation each surrounds one of the
Der zweite Abschnitt 70 der Abstützelemente 50 ist in das vordere Ende (d.h. welches sich in Richtung des ersten Rotorendes 16 bzw. in Richtung des zweiten Rotorendes 18 befindet) der Trägerplatte der Wickelstützelemente integriert, um hierdurch die Enden dieser Trägerplatte gegen die radial wirkenden Kräfte des Drahtzuges der Wicklung zu stützen.The
Claims (6)
- Rotor (1) for an electrodynamic machine, in particular an electric motor, containing:- a rotor assembly (10) with a first rotor end (16) and a second rotor end (18), as well as a plurality of interconnected lamination rings (20), each lamination ring (20) containing at least one web element (22) and the web elements (22) positioned in series forming a web (30), and- web insulation with at least one winding support element for receiving a rotor coil,wherein the winding support elements surround the webs (30) of the rotor assembly (10) and have an elongated base body with a carrier plate,
wherein at least one end lamination element (40) is provided with at least one support element (50), wherein the end lamination element (40) is arranged at least partly in the winding support element and wherein the support element (50) contains a first section (60) and a second section (70), the first section (60) extending substantially in a first plane and the second section (70) extending substantially in a second plane perpendicular to the first plane and in the direction of a rotor end (16, 18) so that the first section (60) of the support elements (50) supports the webs (30) against the axially acting forces generated by the wire tension of the winding and so that the second section (70) of the support elements (50) is integrated into the front end of the carrier plate of the winding support elements in order thereby to protect the ends of this carrier plate against the radially acting forces of the wire tension of the winding. - Rotor (1) according to claim 1, characterised in that the end lamination element (40) is positioned at the first rotor end (16).
- Rotor (1) according to claim 1, characterised in that the first section (60) of the support element (50) is positioned on an end face of a web (30).
- Rotor (1) according to claim 1 or claim 3, characterised in that a stiffening element is provided between the first section (60) and the second section (70) of the support element.
- Rotor (1) according to one of claims 1 to 4, characterised in that the support element (50) is designed in the form of a curved contour, a free end of the support element extending in the direction of a rotor end (16, 18).
- Rotor (1) according to one of claims 1 to 5, characterised in that the end lamination element (40) is formed of a higher-strength material.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102012223977.4A DE102012223977A1 (en) | 2012-12-20 | 2012-12-20 | Rotor package with function carrier |
PCT/EP2013/076822 WO2014095802A2 (en) | 2012-12-20 | 2013-12-17 | Rotor assembly having a functional carrier |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2936656A2 EP2936656A2 (en) | 2015-10-28 |
EP2936656B1 true EP2936656B1 (en) | 2017-06-07 |
Family
ID=49816920
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP13810933.5A Active EP2936656B1 (en) | 2012-12-20 | 2013-12-17 | Rotor assembly having a functional carrier |
Country Status (5)
Country | Link |
---|---|
US (1) | US9979252B2 (en) |
EP (1) | EP2936656B1 (en) |
CN (1) | CN104969450A (en) |
DE (1) | DE102012223977A1 (en) |
WO (1) | WO2014095802A2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102022127293A1 (en) | 2022-10-18 | 2024-04-18 | Audi Aktiengesellschaft | Pole cover for an electric motor |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9893584B2 (en) * | 2015-06-24 | 2018-02-13 | Hamilton Sundstrand Corporation | End winding support for an electric generator |
FR3048566A1 (en) * | 2016-03-02 | 2017-09-08 | Valeo Equip Electr Moteur | ROTOR OF ELECTRIC MACHINE |
CN106849451B (en) * | 2016-12-25 | 2023-03-24 | 中船重工电机科技股份有限公司 | Star-shaped contact ring structure of rotor winding of doubly-fed asynchronous wind generator |
FR3080232B1 (en) * | 2018-04-12 | 2021-12-24 | Renault Sas | SYNCHRONOUS ELECTRIC MACHINE ROTOR OF COIL ROTOR TYPE. |
DE102021209866A1 (en) | 2021-09-07 | 2023-03-09 | Mahle International Gmbh | inner rotor |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3831268A (en) * | 1973-12-03 | 1974-08-27 | Briggs & Stratton Corp | Method of making an electric motor armature core |
GB2290172B (en) * | 1991-09-04 | 1996-04-10 | Onan Corp | A collector ring assembly |
DE19964061A1 (en) * | 1999-12-30 | 2001-07-05 | Bosch Gmbh Robert | Electric motor, in particular for hand machine tools |
WO2008105054A1 (en) | 2007-02-26 | 2008-09-04 | Mitsubishi Electric Corporation | Stator of motor and motor and pump and method for manufacturing motor |
TWI504107B (en) * | 2010-09-10 | 2015-10-11 | Delta Electronics Inc | Silicon steel assembly and method for assembling thereof |
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2012
- 2012-12-20 DE DE102012223977.4A patent/DE102012223977A1/en not_active Withdrawn
-
2013
- 2013-12-17 CN CN201380072383.7A patent/CN104969450A/en active Pending
- 2013-12-17 US US14/654,396 patent/US9979252B2/en active Active
- 2013-12-17 WO PCT/EP2013/076822 patent/WO2014095802A2/en active Application Filing
- 2013-12-17 EP EP13810933.5A patent/EP2936656B1/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102022127293A1 (en) | 2022-10-18 | 2024-04-18 | Audi Aktiengesellschaft | Pole cover for an electric motor |
Also Published As
Publication number | Publication date |
---|---|
CN104969450A (en) | 2015-10-07 |
US9979252B2 (en) | 2018-05-22 |
EP2936656A2 (en) | 2015-10-28 |
US20150349601A1 (en) | 2015-12-03 |
WO2014095802A3 (en) | 2014-12-11 |
DE102012223977A1 (en) | 2014-06-26 |
WO2014095802A2 (en) | 2014-06-26 |
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